Design and Construction Flashcards

1
Q

MD500D is a _____ place ______ hand pilot seat aircraft.

A

5 place

Left Hand

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2
Q

Main Rotor is a ______ _______ system with ______ Blades.

A

Fully articulated system

5 Blades

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3
Q

Anti torque is provided by ______ bladed ______ _______ system.

A

2 bladed

semi rigid

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4
Q

Fuselage is a ______ _______ structure divided into _______ main sections

A

Semi-Monocoque

3 main sections

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5
Q

________ charged landing gear dampers act as _______ ________ and provide ________ resonance stability

A

Nitrogen
Shock absorbers
Ground resonance

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6
Q

What is the Rolls-Royce 250-C20B Horsepower rating and derating?

A

420 SHP
375 SHP at 103% N2 Rpm Take Off
355 SHP MCP

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7
Q

How does the engine oil cooler operate?

A

Belt driven off the main drive shaft and draws air from inlet fairing. Supplies cooling air to engine, transmission oil coolers and engine compartment

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8
Q

Main rotor system incorporates _______ steps to deal with blade _______ loading and allow __________

A

3 steps
centrifugal
feathering

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9
Q

Strap Configuration allows centrifugal load exerted by one blade to be countered by force exerted by _____ ______ blades.

A

2 opposite blades

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10
Q

The V-legs of _______ pack rotate as driving members to turn blades

A

Strap

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11
Q

Straps on main rotor are configured to?

A

To allow feathering and flapping of the blades

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12
Q

_______ cyclic trim actuators allow flight loads to be trimmed out.

A

Electric

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13
Q

Does the MD500D incorporate hydraulic boost pumps?

A

No stick control forces are low

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14
Q

Auto re ignition system power is supplied through the _______ _____ circuit breaker and system is armed by ______ _______ _________ oil pressure

A

ENG OUT

Main Rotor Transmission

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15
Q

Auto re ignition system is activated by ______ N1 or _____ Nr and also activates the ____ _____ _____ _____ warning

A

55% N1
468 Nr
ENG OUT low rotor warning

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16
Q

Auto Re ignition light must be _____ reset after N1 and Nr increase above _________

A

55% N1/468 Nr